Oscillatory aerodynamic forces for a pitching aircraft

  • R. R. Aggarwal Office Of The D.C.S.O. (Air), New Delhi
Keywords: Bending-torsion, Aerodynamic strip, Oscillations

Abstract

Chordwise aerodynamic strip derivatives for the swept back wing having bending-torsion degrees of freedom as modified by the aircraft simple harmonic pitching oscillations have been calculated.
Published
2014-03-25
How to Cite
Aggarwal, R. (2014). Oscillatory aerodynamic forces for a pitching aircraft. Defence Science Journal, 11(1), 12-14. https://doi.org/10.14429/dsj.11.6789
Section
Research Papers